W DOC AIRBUS | AMM A320F

Operational Test of the Passenger Call Lamps through the MCDU


TASK 23-73-00-710-033-A
Operational Test of the Passenger Call Lamps through the MCDU


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 23-73-00-861-001-A
Energize the Cabin Intercommunication Data System (CIDS)
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 31-32-00-860-003-A
Procedure to Get Access to the SYSTEM REPORT/TEST/COM Page
TASK 31-60-00-860-001-A
EIS Start Procedure
TASK 31-60-00-860-002-A
EIS Stop Procedure
3. Job Set-up
Subtask 23-73-00-860-150-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) Make sure that the Cabin Intercommunication Data System (CIDS) is energized
(Ref. AMM TASK 23-73-00-861-001).
   (3) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
   (4) Energize the Centralized Fault Display System (CFDS)
(Ref. AMM TASK 31-32-00-860-003).
   (5) Make sure that a minimum of one cabin door is open.
Subtask 23-73-00-865-169-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUENGINE/2/FADEC A/AND EIU 22KS2A05
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
49VUL/G/LGCIU/SYS1/NORM1GAC09
49VUAIR COND/SDCU/CHAN111WQC06
49VUAIR COND/CAB/PRESS/CTL11HLD09
121VUENGINE/ENG2/FADEC B4KS2Q40
121VUHYDRAULIC/LGCIU/SYS22GAQ35
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
122VUAIR COND/SDCU/CHAN212WQT18
122VUAIR COND/CAB PRESS/CTL/22HLY22
4. Procedure
Subtask 23-73-00-710-296-A ** ON A/C NOT FOR ALL
A. Do this test
ACTION
RESULT
1.On the CFDS-MCDU:
On the CFDS-MCDU:
  • push the MCDU MENU pushbutton.
  • the MCDU MENU page shows.
  • push the CFDS related line select key.
  • the CFDS page shows.
  • push the SYSTEM REPORT/TEST line select key.
  • the SYSTEM REPORT/TEST page shows.
  • push the COM related line select key.
  • the SYSTEM REPORT/TEST COM page shows.
  • push the CIDS1 related line select key.
  • the CIDS1 (ACT) page shows.
  • push the TEST related line select key.
  • the CIDS1 (ACT) TEST page shows.
  • push and release the NEXT PAGE pushbutton until the PAX CALL LAMPS test is indicated.

  • push the PAX CALL LAMPS related line select key.
  • the CIDS1 (ACT) PAX CALL LAMPS TEST page with the message TEST IN PROGRESS shows.

  • after some seconds the message TEST IN PROGRESS changes to TEST OK.
NOTE: An incorrect FAULT message will be recorded for each LED (without bulbs) PAX CALL LAMP, if the test of the related lamps is not deactivated in the CAM.
  • push the MCDU MENU pushbutton.
  • the MCDU MENU page shows.
5. Close-up
Subtask 23-73-00-860-151-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
[Rev.10 from 2021] 2026.04.05 10:34:39 UTC